|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/321 ; 102/384 ; 102/388 ; 244/328|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 23 인용 특허 : 2|
A missile on-board flight pitch, yaw and roll control drag actuator system. The system having a plurality of control panels operated by an actuator drive. The actuator drive accurately positioning the panels in a desired position in the airstream of the missile for controlling the flight, orientation and speed of the aircraft.
An on-board flight pitch, yaw and roll control drag actuator system for controlling the flight of a missile, the system comprising: a plurality of control panels hinged on the missile; an actuator connected to each pannel for opening and closing the panels into the airstream of the missile, the actuator connected to the panel using a two-way actuator drive with a gas operated piston mounted therein, the piston having an actutor rod extending outwardly therefrom, the end of the actuator rod connected to a slide lever attached to a hinged joint mounted at ...